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Airplane Model Detials


General Data

Manufacturer
Avions Pierre Robin
Model
DR 400/200
Comment
Kennblatt Nr. 1001
Modified UTC
2020-06-06 16:03:55

Speed

Vne (NEVER EXCEED)166 Kt
308 KMH
Vno (max. cruise)
140 Kt
260 KMH
Va (maneuver IAS)116 Kt
215 KMH
Vfe (max. speed with extended flaps) 92 Kt
170 KMH

Do not exceed Vno speed except in smooth air, and then only with caution


Flaps


Vfe (max. speed)Vat (app. speed)
2nd pos.92 Kt / 170 KMH65 Kt / 120 KMH


Climb Performance


Flaps at T/OFlaps retracted
Vx (best ANGLE of climb)78 Kt / 145 KMH86 Kt / 160 KMH
Vy (best RATE of climb)
65 Kt / 120 KMH
67 Kt / 125 KMH


Best glide speed:

Flaps retracted: 81 Kt / 150 KMH, glide factor 1:9.3


Stall

Weight 1100 Kg (2325 lbs), Idle


Kt / KMH IAS
Bank Angle0
3060
Flaps retracted
56 Kt / 104 KMH
60 Kt / 112 KMH
79 Kt / 147 KMH
Flaps T/O (pos. 1)
53 Kt / 98 KMH
57 Kt / 105 KMH
75 Kt / 139 KMH
Flaps LND (pos. 2)
49 Kt / 91 KMH
53 Kt / 98 KMH
69 Kt / 127 KMH


Take-Off Performance

Max. weight: 1100 Kg (2425 lbs), dry asphalt, no wind, Flaps T/O, Full Throttle, no incl., cooling open

Take-Off Speed: 61 Kt / 113 KMH

IAS in 15 m / 50 ft height: 68 Kt / 127 KMH


Landing Performance

Max. weight: 1100 Kg (2425 lbs), dry asphalt, no wind, Flaps LND, Idle, no incl.

IAS in 15 m / 50 ft height: 63 Kt / 117 KMH

Landing Speed: 51 Kt / 95 KMH


Engine Performance

 

Max T/O Power 5 min

2700 RPM

Max Continuous Power

2500 RPM

Max. starting time
30 sec
Max. cylinder head temp.
260 C / 500 F


G-Factors for N-Category

max negative

max positive

Flaps retracted

-1.9

+3.8

Flaps extended

0.0

+2.0

Data for CG calculation














Seats
Tanks
Trunks

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